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基于线性参变模型的大包线飞行控制系统设计 被引量:3

Linear Parameter Varying Modeling Techniques for Large Envelope Flight Control System
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摘要 介绍一种基于线性参变模型(LPV)设计大包线飞行控制器的新方法。这种设计方法是应用基于LMI的H_∞控制来设计飞行控制器,能够从理论确保飞行控制系统的稳定性和鲁捧性。文中主要研究基于单一Lyapuanov方程的LPV自增益调参控制器的设计方法。 A new approach based on LPV model to design large envelope flight control system is presented.Because the approach which is based on LMI's H-infinity control technique is made use of designing flight control system,it can guarantee stabilization and robust perferance of flight control system in theory.Single quadratic Lyapunov function based on H_∞theory was introduced on this paper.
作者 武晓光 刘林
出处 《弹箭与制导学报》 CSCD 北大核心 2006年第S2期353-356,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 大包线 线性参变模型(LPV) H_∞控制 线性矩阵不等式(LMI) large envelope linear parameter varying model infinity control linear matrix inequality
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参考文献6

  • 1Paul Blue,Levent Giivenc,and Dirk Odenhal.Robustness and performance specifications[].Proceedings of the American Control Confercnce.2001
  • 2Abhishek Kumsr,and Mark R.Anderson.A companrison of LPV modeling techniques for air- cart control[].AIAA —.
  • 3Lawton H.Lee,and Mark Spillman.Control of slowly varying LPV systems-An application to flight control-linear parameter varying[].AIAA——.
  • 4Jong-Yeob Shin,Gary J.Balas,and Alpay M, Kaya.Blending approach of linear parameter var- ying control synthesis for F-16 aircraft[].AIAA——.
  • 5Jonathan Protz,and Andrew Sparks.An LPV con- troller for a tailless fighter aircraft simulation[].AIAA——.
  • 6Andcr G.Sparks.Linear parameter varying con- trol for a tailless aircraft. AIAA-00-37156 .

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